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2009 Annual Report - NASA Airborne Science Program

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AAFEx<br />

HQ sponsor: Aeronautics Research Mission Directorate<br />

During January and February <strong>2009</strong> the DC-8 was<br />

employed in a ground test series to support the<br />

Alternative Aviation Fuel Experiment (AAFEX)<br />

at the <strong>NASA</strong> Dryden Aircraft Operations Facility<br />

(DAOF) in Palmdale, California. The rising cost of<br />

oil coupled with the need to reduce pollution and<br />

dependence on foreign suppliers has spurred great<br />

interest and activity in developing alternative aviation<br />

fuels. Detailed studies are required to ascertain the<br />

exact impacts of the fuels on engine operation and<br />

exhaust composition. In response to this need,<br />

<strong>NASA</strong> acquired candidate alternative fuels from a<br />

variety of sources and burned the fuels in the <strong>NASA</strong><br />

DC-8 to assess changes in the aircraft’s CFM-56<br />

engine performance and emission parameters<br />

relative to operation with standard JP-8. The<br />

AAFEX Aeronautics Research Mission Directorate<br />

project managed by Dan Bulzan of <strong>NASA</strong> Glen<br />

Research Center and under the direction of the<br />

Project Lead Scientist Bruce Anderson of <strong>NASA</strong><br />

Langley Research Center, the AAFEX tests sought<br />

to establish fuel matrix effects on: 1) engine and<br />

exhaust gas temperatures and compressor speeds and<br />

pressures; 2) engine and auxiliary power unit (APU)<br />

gas phase and particle emissions and characteristics;<br />

and 3) volatile aerosol formation in aging exhaust<br />

plumes. A secondary goal of the study was to<br />

evaluate the role of ambient conditions in regulating<br />

volatile aerosol emissions. Gas phase measurements<br />

included the standard certification species (CO 2 , CO,<br />

NO x , and THC) along with hydrocarbons, hazardous<br />

air pollutants (HAPS), and oxygenated compounds.<br />

Measured particle parameters included smoke<br />

number; number density, size distribution and total<br />

Figure 30:<br />

Arial view of the AAFEX test setup showing DC-8 in the open-air engine run-up<br />

facility at the Dryden Aircraft Operations Facility in Palmdale, CA.<br />

33

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